View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61638U 26145.53314179 +.00000000 +00000-0 -14416-3 0 00008
2 61638 43.0003 84.4281 0000868 265.0045 95.0707 15.27571476 00
| Epoch (UTC): | 25 May 2026 12:47:43 |
| Eccentricity: | 0.0000868 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.4281° |
| argument of perigee: | 265.0045° |
| revolutions per day: | 15.27571476 |
| mean anomaly at epoch: | 95.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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